चैनल - STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK / :: Library Catalog

समान संसाधन: STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /

त्वरित देखें
EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOILEXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL
त्वरित देखें
COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW VELOCITY AND DIRECTION AROUND NACA 0012 & NACA 0015 AIRFOIL
त्वरित देखें
A COMPARATIVE STUDY OF AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 4415 AIRFOILS AT VARIOUS REYNOLDS NUMBER /
त्वरित देखें
A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND NACA 4418 AND NACA 0012 AIRFOIL /
त्वरित देखें
SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
त्वरित देखें
STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS AND IMPROVED PERFORMANCE OF NACA 0015 AIRFOIL WITH BLEED /
त्वरित देखें
"INFLUENCE OF SURFACE MODIFICATION ON THE LIFT-DRAG CHARACTERISTICS OF NACA 0012 AIRFOIL" /
त्वरित देखें
PERFORMANCE ANALYSIS OF FIXED AND MORPHING WINGS USING NACA 4412 ASYMMETRIC AIRFOILS UNDER VARYING ANGLES OF ATTACK AND FLOW REGIMES /
त्वरित देखें
FLOW CHARACTERISTICS AND HEAT TRANSFER CHARACTERISTICS OVER NACA 4415 AIRFOIL
त्वरित देखें
CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
त्वरित देखें
STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
त्वरित देखें
STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS BETWEEN DIFFERENT CONFIGURATIONS OF THREE DIMENSIONAL MODELS OF NACA 4412 AIRFOIL /
त्वरित देखें
ANALYSIS OF FLOW DYNAMICS OF A NACA 2412 AIRFOIL WITH CAVITY THROUGH NUMERICAL SIMULATION AND WIND TUNNEL EXPERIMENT /
त्वरित देखें
A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
त्वरित देखें
AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
त्वरित देखें
COMPARATIVE AND ASSESSMENT OF VARIOUS TURBULENCE MODELS AND IMPROVED PERFORMANCE OF NACA 0010 AIRFOIL WITH MSBLC /
त्वरित देखें
EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS OF ROUGHENED SURFACE AIRFOILS /
त्वरित देखें
EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF THE CHARACTERISTICS OF NACA 4412 AEROFOIL USING DIFFERENT SHAPES /
त्वरित देखें
PREDICTION OF ICE ACCRETION AND CFD ANALYSIS OF NACA 2412 AIRFOIL FOR EVALUATION OF AERODYNAMIC PERFORMANCE DEGRADATION /
त्वरित देखें
EXPERIMENTAL STUDY OF THE FLOW FIELD OF AN ANNULAR JET COALESCING AT THE EXIT /
त्वरित देखें
ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/

विषय: Aeronautical Engineering.

विषय: This Thesis Paper of AE in B.Sc. Program.

लेखक: Sharna, Sayema Salim

त्वरित देखें
STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /

लेखक: Rakib, Md. Sanower Hossen

त्वरित देखें
STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /